View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00005U 26037.21040462 +.00000000 +00000-0 +17127-3 0 00006
2 00005 34.2621 358.5266 1839380 267.9177 71.0902 10.85947394 00
| Epoch (UTC): | 06 February 2026 05:02:58 |
| Eccentricity: | 0.1839380 |
| inclination: | 34.2621° |
| perigee height: | 651 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 358.5266° |
| argument of perigee: | 267.9177° |
| revolutions per day: | 10.85947394 |
| mean anomaly at epoch: | 71.0902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|